View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62530U 26145.48048772 +.00000000 +00000-0 +56064-3 0 00001
2 62530 43.0007 146.1171 0002271 269.6978 90.3614 15.27589458 09
| Epoch (UTC): | 25 May 2026 11:31:54 |
| Eccentricity: | 0.0002271 |
| inclination: | 43.0007° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 146.1171° |
| argument of perigee: | 269.6978° |
| revolutions per day: | 15.27589458 |
| mean anomaly at epoch: | 90.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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